EP 2977679 B1 20190828 - COMBUSTOR WALL FOR A GAS TURBINE ENGINE AND METHOD OF ACOUSTIC DAMPENING
Title (en)
COMBUSTOR WALL FOR A GAS TURBINE ENGINE AND METHOD OF ACOUSTIC DAMPENING
Title (de)
BRENNKAMMERWAND FÜR EINEN GASTURBINENMOTOR UND VERFAHREN ZUR AKUSTISCHEN DÄMPFUNG
Title (fr)
PAROI DE CHAMBRE DE COMBUSTION POUR UN MOTEUR À TURBINE À GAZ ET PROCÉDÉ D'AMORTISSEMENT ACOUSTIQUE
Publication
Application
Priority
US 201462027506 P 20140722
Abstract (en)
[origin: EP2977679A1] A vascular wall (58, 60) of a combustor that may be for a gas turbine engine includes a first face defining at least in-part a combustion chamber (64), a second face defining at least in-part a cooling air plenum (68), and a vascular lattice structure (108) located between the first and second faces for distributing cooling air from the plenum (68) and to the chamber (64). The vascular lattice structure (108) may be configured to enhance cooling air flow where needed while providing structural support. The orientation of the vascular lattice structure (108) may further contribute toward acoustic dampening.
IPC 8 full level
F23R 3/00 (2006.01); F23M 20/00 (2014.01); F23R 3/04 (2006.01)
CPC (source: EP US)
F02C 7/24 (2013.01 - US); F23M 20/005 (2015.01 - EP US); F23R 3/002 (2013.01 - EP US); F23R 3/04 (2013.01 - US); F23R 2900/00014 (2013.01 - EP US); F23R 2900/03042 (2013.01 - EP US); F23R 2900/03043 (2013.01 - US); Y02T 50/60 (2013.01 - EP US)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
EP 2977679 A1 20160127; EP 2977679 B1 20190828; US 10371381 B2 20190806; US 2016153658 A1 20160602
DOCDB simple family (application)
EP 15177926 A 20150722; US 201514805963 A 20150722